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Experimental investigation of a turbulent boundary layer at mach 6, high reynolds numbers, and zero heat transferTurbulent boundary layer on hollow cylinder at Mach 6, high Reynolds number, and zero heat transfer
Document ID
19650020242
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Adcock, J. B. (NASA Langley Research Center Hampton, VA, United States)
Mc Ree, D. I. (NASA Langley Research Center Hampton, VA, United States)
Peterson, J. B., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1965
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TN-D-2907
Report Number: NASA-TN-D-2907
Accession Number
65N29843
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TURBULENT BOUNDARY LAYER
HEAT TRANSFER
CYLINDER
REYNOLDS NUMBER

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